View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63940U 26145.23751193 +.00000000 +00000-0 -20377-3 0 00007
2 63940 70.0009 81.6447 0003025 262.6054 97.4761 14.98330768 08
| Epoch (UTC): | 25 May 2026 05:42:01 |
| Eccentricity: | 0.0003025 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.6447° |
| argument of perigee: | 262.6054° |
| revolutions per day: | 14.98330768 |
| mean anomaly at epoch: | 97.4761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|